DE60302861D1 - A system using an indication of control vibration clutches for electrical flight control of an aircraft, and control for such a system - Google Patents

A system using an indication of control vibration clutches for electrical flight control of an aircraft, and control for such a system

Info

Publication number
DE60302861D1
DE60302861D1 DE60302861T DE60302861T DE60302861D1 DE 60302861 D1 DE60302861 D1 DE 60302861D1 DE 60302861 T DE60302861 T DE 60302861T DE 60302861 T DE60302861 T DE 60302861T DE 60302861 D1 DE60302861 D1 DE 60302861D1
Authority
DE
Germany
Prior art keywords
control
pilot
clutches
aircraft
indication
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60302861T
Other languages
German (de)
Other versions
DE60302861T2 (en
Inventor
Nathalie Raimbault
Jean-Pierre Gautier
Alain Sagansan
Pierre Fabre
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Application granted granted Critical
Publication of DE60302861D1 publication Critical patent/DE60302861D1/en
Publication of DE60302861T2 publication Critical patent/DE60302861T2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Vibration Prevention Devices (AREA)
  • Vehicle Body Suspensions (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Details Of Aerials (AREA)
  • Toys (AREA)
  • Mechanical Control Devices (AREA)
  • Position Input By Displaying (AREA)

Abstract

Pilot commands from a joystick (2) are captured by sensors (4,6) and sent to a calculator (7) which causes actuators (12) to move control surfaces (10). Integral attenuation units (13,14) prevent a too rapid joystick operation and additional controllable attenuation units (15,16) are started by a pilot induced oscillation detector in the calculator and may operate constantly or in proportion to the amount of oscillation. An Independent claim is also included for a pilot control which includes means of detecting pilot induced oscillations and initiating the operation of controllable attenuation units.
DE60302861T 2002-11-18 2003-10-23 A system using an indication of control vibration clutches for electrical flight control of an aircraft, and control for such a system Expired - Lifetime DE60302861T2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0214388 2002-11-18
FR0214388A FR2847352B1 (en) 2002-11-18 2002-11-18 AIRCRAFT FLIGHT CONTROL SYSTEM FOR AIRCRAFT HAVING DETECTION OF OSCILLATORY STEERING COUPLINGS AND STEERING BODY FOR SUCH A SYSTEM

Publications (2)

Publication Number Publication Date
DE60302861D1 true DE60302861D1 (en) 2006-01-26
DE60302861T2 DE60302861T2 (en) 2006-08-03

Family

ID=32116638

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60302861T Expired - Lifetime DE60302861T2 (en) 2002-11-18 2003-10-23 A system using an indication of control vibration clutches for electrical flight control of an aircraft, and control for such a system

Country Status (6)

Country Link
US (2) US20050021193A1 (en)
EP (1) EP1420320B1 (en)
AT (1) ATE313823T1 (en)
CA (1) CA2447283C (en)
DE (1) DE60302861T2 (en)
FR (1) FR2847352B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2821603C1 (en) * 2023-09-11 2024-06-25 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Method of damping impact to electric drive

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2847353B1 (en) * 2002-11-18 2006-07-14 Airbus France METHOD AND DEVICE FOR DETECTION OF OSCILLATORY STEERING COUPLINGS IN AN AIRCRAFT
US7272473B2 (en) * 2004-09-17 2007-09-18 The Boeing Company Methods and systems for analyzing system operator coupling susceptibility
FR2889162B1 (en) 2005-07-28 2007-09-07 Airbus France Sas METHOD AND DEVICE FOR DRIVING AN AIRCRAFT ACCORDING TO AT LEAST ONE AXIS OF DRIVING
DE202008005918U1 (en) * 2008-04-29 2009-09-03 Jungheinrich Aktiengesellschaft Actuator arrangement for control organs
FR2980453B1 (en) * 2011-09-26 2014-06-27 Airbus Operations Sas STEERING CONTROL ELECTRONIC SYSTEM FOR AIRCRAFT
WO2013074134A1 (en) * 2011-11-17 2013-05-23 National Institute Of Aerospace Associates Radiation shielding materials containing hydrogen, boron and nitrogen
JP6433134B2 (en) 2013-03-19 2018-12-05 株式会社ディ・アンド・ディ Coating type radiation shielding material
US10482783B2 (en) 2015-11-06 2019-11-19 Frasca International, Inc. Adaptive assistance for flight simulation
CN106741870B (en) * 2016-11-30 2019-03-26 中国直升机设计研究所 A kind of cockpit steerable system and method
FR3086273B1 (en) * 2018-09-26 2020-10-09 Safran Electronics & Defense AIRCRAFT FLIGHT CONTROL DEVICE
CN114044125B (en) * 2021-12-21 2024-05-14 中国商用飞机有限责任公司 Aircraft manipulation control system and control method

Family Cites Families (18)

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Publication number Priority date Publication date Assignee Title
US3236478A (en) * 1964-04-23 1966-02-22 North American Aviation Inc Flight control system
US4030011A (en) * 1975-03-24 1977-06-14 Honeywell Inc. Multimode control systems
DE2807902C2 (en) * 1978-02-24 1980-04-30 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Control device with active force feedback
US4298833A (en) * 1980-02-29 1981-11-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus for damping operator induced oscillations of a controlled system
US4477043A (en) * 1982-12-15 1984-10-16 The United States Of America As Represented By The Secretary Of The Air Force Biodynamic resistant control stick
DE3431583A1 (en) * 1984-08-28 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn DEVICE FOR THE AUTOMATIC ELIMINATION OF TAX FORCE ERRORS IN AIRCRAFT, IN PARTICULAR HELICOPTERS
USH703H (en) * 1987-07-30 1989-11-07 The United States Of America As Represented By The Secretary Of The Air Force Manual control apparatus with electable mechanical impedance
FR2643502B1 (en) * 1989-02-20 1996-01-19 Aerospatiale SWITCHING HANDLE CONTROL DEVICE, PARTICULARLY FOR AIRCRAFT, AND SYSTEM COMPRISING SUCH A DEVICE
US5076517A (en) * 1989-08-14 1991-12-31 United Technologies Corporation Programmable, linear collective control system for a helicopter
US5107080A (en) * 1989-12-01 1992-04-21 Massachusetts Institute Of Technology Multiple degree of freedom damped hand controls
FR2756392B1 (en) * 1996-11-22 1999-01-22 Aerospatiale CONTROL SLEEVE COUPLING SYSTEM
US5935177A (en) * 1997-02-06 1999-08-10 Accurate Automation Corporation Pilot-induced oscillation detection and compensation apparatus and method
US6325331B1 (en) * 1998-12-11 2001-12-04 Bell Helicopter Textron Inc. Trim actuator
US6199028B1 (en) * 1999-02-04 2001-03-06 The United States Of America As Represented By The Secretary Of The Air Force Detector for human loss of tracking control
US6311110B1 (en) * 1999-06-17 2001-10-30 Lord Corporation Adaptive off-state control method
US6459228B1 (en) * 2001-03-22 2002-10-01 Mpc Products Corporation Dual input servo coupled control sticks
US20030183728A1 (en) * 2002-03-29 2003-10-02 The Boeing Company Aircraft control surface controller and associated method
US20040078120A1 (en) * 2002-10-16 2004-04-22 Edgar Melkers Non-linear compensation of a control system having an actuator and a method therefore

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2821603C1 (en) * 2023-09-11 2024-06-25 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Method of damping impact to electric drive

Also Published As

Publication number Publication date
EP1420320B1 (en) 2005-12-21
EP1420320A1 (en) 2004-05-19
CA2447283A1 (en) 2004-05-18
ATE313823T1 (en) 2006-01-15
DE60302861T2 (en) 2006-08-03
US8473121B2 (en) 2013-06-25
CA2447283C (en) 2012-04-24
FR2847352B1 (en) 2005-01-28
US20050021193A1 (en) 2005-01-27
FR2847352A1 (en) 2004-05-21
US20100200701A1 (en) 2010-08-12

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